Commonwealth legislation

AD/CF700/8 - Fan Centre Vent System

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This directive requires owners, operators and maintenance organisations of CF700-2C/‑2D/‑2D‑2 engines to carry out the fan‑centre vent modification/inspection per General Electric Service Bulletin CF700 79‑8 (or AD/GE‑T/20). Work must be completed before the engine’s next installation after any hot‑end inspection or engine reconditioning carried out after 28 January 1972. It matters because it creates a mandatory, event‑triggered maintenance action, shifting cost, scheduling and record‑keeping burdens to operators and independent shops.

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Current sections

Direct links to the current provisions in AD/CF700/8 - Fan Centre Vent System.

AD/CF700/8 - Fan Centre Vent System

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 106 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source General Electric Turbine Engines - CF700 Series

AD/CF700/8 Fan Centre Vent System 9/85

Applicability: All CF700-2C, -2D and -2D-2. Document: General Electric SB (CF700) 79-8; or

AD/GE-T/20.

Compliance: Before installation in an aircraft following next hot end inspection or engine reconditioning completed after 28 January 1972, whichever occurs first.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.